RL-10A-4-2

Summary

RL-10A-4-2 is an engine model^[1].

Key Facts

• RL-10A-4-2's instance of is recorded as engine model^[2].
• RL-10A-4-2's manufacturer is recorded as Pratt & Whitney^[3].
• RL-10A-4-2's subclass of is recorded as RL-10A^[4].
• RL-10A-4-2's country of origin is recorded as United States^[5].
• RL-10A-4-2's first flight is recorded as +2002-00-00T00:00:00Z^[6].
• RL-10A-4-2's source of energy is recorded as liquid oxygen^[7].
• RL-10A-4-2's source of energy is recorded as liquid hydrogen^[8].
• RL-10A-4-2's length is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+2.29'}^[9].
• RL-10A-4-2's mass is recorded as {'unit': 'http://www.wikidata.org/entity/Q11570', 'amount': '+167.8'}^[10].
• RL-10A-4-2's maximum thrust is recorded as {'unit': 'http://www.wikidata.org/entity/Q56402798', 'amount': '+99.2'}^[11].
• RL-10A-4-2's diameter is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+1.53'}^[12].
• RL-10A-4-2's specific impulse by weight is recorded as {'unit': 'http://www.wikidata.org/entity/Q11574', 'amount': '+451'}^[13].

Body

Physical Characteristics

RL-10A-4-2's length is recorded as {'unit': 'http://www.wikidata.org/entity/Q11573', 'amount': '+2.29'}^[9].

Designation and Status

RL-10A-4-2's instance of is recorded as engine model^[2].